Free-falling autorotating plate - A coupled fluid and flight mechanics problem

A computational method coupling the three-degrees-of-freedom flight mechanics equations and the two-dimensional, time-dependent Navier-Stokes equations was developed which could be used to predict the autorotating characteristics of a free-falling, two-dimensional flat plate. The system of ordinary...

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Veröffentlicht in:Journal of aircraft 1985-11, Vol.22 (11), p.983-987
Hauptverfasser: Gallaway, C.R, Hankey, W.L
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container_issue 11
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container_title Journal of aircraft
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creator Gallaway, C.R
Hankey, W.L
description A computational method coupling the three-degrees-of-freedom flight mechanics equations and the two-dimensional, time-dependent Navier-Stokes equations was developed which could be used to predict the autorotating characteristics of a free-falling, two-dimensional flat plate. The system of ordinary differential equations describing the flight mechanics was solved using an Adams-Bashforth explicit method to predict the movement of the plate. New values of the boundary conditions for the Navier-Stokes equations solver were obtained from this movement of the plate. The process was repeated to advance the solution in time. The flight path of a free-falling autorotating plate was predicted using the computational procedure and the validity of the overall approach demonstrated by comparison with experiment.
doi_str_mv 10.2514/3.45235
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1533-3868
language eng
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source Alma/SFX Local Collection
subjects aerodynamics
aircraft
fluid dynamics
incompressible flow
Navier Stokes equations
numerical analysis
title Free-falling autorotating plate - A coupled fluid and flight mechanics problem
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